GB0108398D0 - Seal element for sealing a gap and combustion turbine having a seal element - Google Patents

Seal element for sealing a gap and combustion turbine having a seal element

Info

Publication number
GB0108398D0
GB0108398D0 GBGB0108398.9A GB0108398A GB0108398D0 GB 0108398 D0 GB0108398 D0 GB 0108398D0 GB 0108398 A GB0108398 A GB 0108398A GB 0108398 D0 GB0108398 D0 GB 0108398D0
Authority
GB
United Kingdom
Prior art keywords
seal element
gap
components
sealing
leakage
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Ceased
Application number
GBGB0108398.9A
Other languages
English (en)
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Siemens AG
Original Assignee
Siemens AG
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Siemens AG filed Critical Siemens AG
Priority to GBGB0108398.9A priority Critical patent/GB0108398D0/en
Publication of GB0108398D0 publication Critical patent/GB0108398D0/en
Priority to EP02005897A priority patent/EP1247942B1/de
Priority to ES02005897T priority patent/ES2266330T3/es
Priority to AT02005897T priority patent/ATE331874T1/de
Priority to DE60212751T priority patent/DE60212751T2/de
Priority to JP2002100727A priority patent/JP4191946B2/ja
Priority to US10/117,584 priority patent/US6682300B2/en
Priority to CNB021054363A priority patent/CN1320256C/zh
Ceased legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16J—PISTONS; CYLINDERS; SEALINGS
    • F16J15/00—Sealings
    • F16J15/02—Sealings between relatively-stationary surfaces
    • F16J15/06—Sealings between relatively-stationary surfaces with solid packing compressed between sealing surfaces
    • F16J15/10—Sealings between relatively-stationary surfaces with solid packing compressed between sealing surfaces with non-metallic packing
    • F16J15/12—Sealings between relatively-stationary surfaces with solid packing compressed between sealing surfaces with non-metallic packing with metal reinforcement or covering
    • F16J15/121—Sealings between relatively-stationary surfaces with solid packing compressed between sealing surfaces with non-metallic packing with metal reinforcement or covering with metal reinforcement
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
    • F01D11/005—Sealing means between non relatively rotating elements

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Gasket Seals (AREA)
  • Sealing Material Composition (AREA)
  • Sealing Using Fluids, Sealing Without Contact, And Removal Of Oil (AREA)
GBGB0108398.9A 2001-04-04 2001-04-04 Seal element for sealing a gap and combustion turbine having a seal element Ceased GB0108398D0 (en)

Priority Applications (8)

Application Number Priority Date Filing Date Title
GBGB0108398.9A GB0108398D0 (en) 2001-04-04 2001-04-04 Seal element for sealing a gap and combustion turbine having a seal element
EP02005897A EP1247942B1 (de) 2001-04-04 2002-03-14 Spaltdichtung und Gasturbine mit einer solchen Spaltdichtung
ES02005897T ES2266330T3 (es) 2001-04-04 2002-03-14 Elemento estanco para sellar una separacion, y turbina de combustion que incorpora tal elemento estanco.
AT02005897T ATE331874T1 (de) 2001-04-04 2002-03-14 Spaltdichtung und gasturbine mit einer solchen spaltdichtung
DE60212751T DE60212751T2 (de) 2001-04-04 2002-03-14 Spaltdichtung und Gasturbine mit einer solchen Spaltdichtung
JP2002100727A JP4191946B2 (ja) 2001-04-04 2002-04-03 ギャップシール用のシール要素と該要素を持つ燃焼タービン
US10/117,584 US6682300B2 (en) 2001-04-04 2002-04-04 Seal element for sealing a gap and combustion turbine having a seal element
CNB021054363A CN1320256C (zh) 2001-04-04 2002-04-04 用于密封间隙的密封元件以及具有该密封元件的燃气轮机

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GBGB0108398.9A GB0108398D0 (en) 2001-04-04 2001-04-04 Seal element for sealing a gap and combustion turbine having a seal element

Publications (1)

Publication Number Publication Date
GB0108398D0 true GB0108398D0 (en) 2001-05-23

Family

ID=9912208

Family Applications (1)

Application Number Title Priority Date Filing Date
GBGB0108398.9A Ceased GB0108398D0 (en) 2001-04-04 2001-04-04 Seal element for sealing a gap and combustion turbine having a seal element

Country Status (8)

Country Link
US (1) US6682300B2 (de)
EP (1) EP1247942B1 (de)
JP (1) JP4191946B2 (de)
CN (1) CN1320256C (de)
AT (1) ATE331874T1 (de)
DE (1) DE60212751T2 (de)
ES (1) ES2266330T3 (de)
GB (1) GB0108398D0 (de)

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US7291946B2 (en) * 2003-01-27 2007-11-06 United Technologies Corporation Damper for stator assembly
EP1654440B1 (de) * 2003-08-11 2009-01-07 Siemens Aktiengesellschaft Gasturbine mit einem dichtungselement im bereich des leitschaufelkranzes oder des laufschaufelkranzes des turbinenteils
US7090459B2 (en) * 2004-03-31 2006-08-15 General Electric Company Hybrid seal and system and method incorporating the same
US20050242526A1 (en) * 2004-04-30 2005-11-03 Stefan Dahlke Hot gas seal
DE602006002319D1 (de) * 2005-06-16 2008-10-02 Sulzer Metco Us Inc Aluminiumoxid dotierter verschleissbarer keramischer Werkstoff
EP1767835A1 (de) * 2005-09-22 2007-03-28 Siemens Aktiengesellschaft Hochtemperaturfeste Dichtungsanordnung, insbesondere für Gasturbinen
US7631879B2 (en) * 2006-06-21 2009-12-15 General Electric Company “L” butt gap seal between segments in seal assemblies
FR2913718B1 (fr) * 2007-03-15 2009-06-05 Snecma Propulsion Solide Sa Ensemble d'anneau de turbine pour turbine a gaz
JP4938080B2 (ja) 2007-06-12 2012-05-23 パナソニック株式会社 マルチプロセッサ制御装置、マルチプロセッサ制御方法及びマルチプロセッサ制御回路
US7887929B2 (en) * 2007-08-28 2011-02-15 United Technologies Corporation Oriented fiber ceramic matrix composite abradable thermal barrier coating
US20090110546A1 (en) * 2007-10-29 2009-04-30 United Technologies Corp. Feather Seals and Gas Turbine Engine Systems Involving Such Seals
WO2009116898A1 (en) * 2008-03-18 2009-09-24 Volvo Aero Corporation A gas turbine housing component
LU91455B1 (en) * 2008-06-06 2009-12-07 Wurth Paul Sa Gap-filler insert for use with cooling plates for a metallurgical furnace
US8132442B2 (en) * 2008-09-22 2012-03-13 Siemens Energy, Inc. Compressible ceramic seal
US8157511B2 (en) * 2008-09-30 2012-04-17 Pratt & Whitney Canada Corp. Turbine shroud gas path duct interface
US8382436B2 (en) * 2009-01-06 2013-02-26 General Electric Company Non-integral turbine blade platforms and systems
ATE537333T1 (de) * 2009-01-28 2011-12-15 Alstom Technology Ltd Streifendichtung und verfahren zum entwurf einer streifendichtung
US8262345B2 (en) * 2009-02-06 2012-09-11 General Electric Company Ceramic matrix composite turbine engine
US8684680B2 (en) * 2009-08-27 2014-04-01 Pratt & Whitney Canada Corp. Sealing and cooling at the joint between shroud segments
WO2011035798A1 (en) 2009-09-28 2011-03-31 Siemens Aktiengesellschaft Gas turbine nozzle arrangement and gas turbine
US8398090B2 (en) 2010-06-09 2013-03-19 General Electric Company Spring loaded seal assembly for turbines
US8347636B2 (en) * 2010-09-24 2013-01-08 General Electric Company Turbomachine including a ceramic matrix composite (CMC) bridge
US9945484B2 (en) 2011-05-20 2018-04-17 Siemens Energy, Inc. Turbine seals
GB201109143D0 (en) * 2011-06-01 2011-07-13 Rolls Royce Plc Flap seal spring and sealing apparatus
JP5772327B2 (ja) * 2011-07-19 2015-09-02 富士電機株式会社 高温ガス炉の炉心拘束機構
US9140213B2 (en) 2011-12-06 2015-09-22 United Technologies Corporation Leaf spring damper for a turbine engine fuel delivery system
US20130177411A1 (en) * 2012-01-05 2013-07-11 General Electric Company System and method for sealing a gas path in a turbine
US9970311B2 (en) * 2013-03-05 2018-05-15 United Technologies Corporation Consumable assembly tool for a gas turbine engine
US9759081B2 (en) 2013-10-08 2017-09-12 General Electric Company Method and system to facilitate sealing in gas turbines
EP2960439A1 (de) * 2014-06-26 2015-12-30 Siemens Aktiengesellschaft Turbomaschine mit äußerer Dichtung und Verwendung dieser Turbomaschine
US10443423B2 (en) * 2014-09-22 2019-10-15 United Technologies Corporation Gas turbine engine blade outer air seal assembly
DE102014219137A1 (de) * 2014-09-23 2016-03-24 Siemens Aktiengesellschaft Dichtelement für gestufte Teilfugen an Getriebegehäusen
CN104632414A (zh) * 2015-01-30 2015-05-20 北京华清燃气轮机与煤气化联合循环工程技术有限公司 一种燃气轮机用密封结构
US9869201B2 (en) * 2015-05-29 2018-01-16 General Electric Company Impingement cooled spline seal
US20170370239A1 (en) * 2016-06-22 2017-12-28 General Electric Company Turbine systems with sealing components
US10557362B2 (en) * 2017-03-30 2020-02-11 General Electric Company Method and system for a pressure activated cap seal
US11156116B2 (en) 2019-04-08 2021-10-26 Honeywell International Inc. Turbine nozzle with reduced leakage feather seals
CN113623020B (zh) * 2021-08-02 2022-07-08 无锡友鹏航空装备科技有限公司 一种密封性高的涡轮导向装置

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GB1483532A (en) * 1974-09-13 1977-08-24 Rolls Royce Stator structure for a gas turbine engine
GB1493913A (en) * 1975-06-04 1977-11-30 Gen Motors Corp Turbomachine stator interstage seal
US3966356A (en) * 1975-09-22 1976-06-29 General Motors Corporation Blade tip seal mount
US3975114A (en) * 1975-09-23 1976-08-17 Westinghouse Electric Corporation Seal arrangement for turbine diaphragms and the like
US4199151A (en) * 1978-08-14 1980-04-22 General Electric Company Method and apparatus for retaining seals
FR2455674A1 (fr) * 1979-05-02 1980-11-28 Snecma Dispositif d'etancheite entre deux elements de turbomachine
JPS5719283U (de) * 1980-07-08 1982-02-01
US4465284A (en) * 1983-09-19 1984-08-14 General Electric Company Scalloped cooling of gas turbine transition piece frame
US4524980A (en) * 1983-12-05 1985-06-25 United Technologies Corporation Intersecting feather seals for interlocking gas turbine vanes
JPS61164003A (ja) * 1985-01-11 1986-07-24 Hitachi Ltd 流体機械における熱伸びのある静翼部のシ−ル装置
US4645217A (en) * 1985-11-29 1987-02-24 United Technologies Corporation Finger seal assembly
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FR2713709B1 (fr) * 1993-12-08 1996-01-12 Snecma Paroi de turbomachine comprenant un corps d'étanchéité.
US5657998A (en) * 1994-09-19 1997-08-19 General Electric Company Gas-path leakage seal for a gas turbine
JPH08109368A (ja) * 1994-10-11 1996-04-30 Nichias Corp 複合ガスケット
JP3349278B2 (ja) * 1994-11-09 2002-11-20 三菱重工業株式会社 シール構造
JPH08277701A (ja) * 1995-04-04 1996-10-22 Ishikawajima Harima Heavy Ind Co Ltd タービン静翼支持構造
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JPH1162502A (ja) * 1997-08-21 1999-03-05 Ishikawajima Harima Heavy Ind Co Ltd タービン動翼のシールダンパー
US6162014A (en) * 1998-09-22 2000-12-19 General Electric Company Turbine spline seal and turbine assembly containing such spline seal
JP2000104832A (ja) * 1998-09-29 2000-04-11 Nippon Valqua Ind Ltd フッ素樹脂包みガスケット
JP4240428B2 (ja) * 1999-06-08 2009-03-18 電気化学工業株式会社 触媒コンバータのシール材の製造方法

Also Published As

Publication number Publication date
DE60212751D1 (de) 2006-08-10
US20020168263A1 (en) 2002-11-14
ATE331874T1 (de) 2006-07-15
CN1320256C (zh) 2007-06-06
EP1247942A3 (de) 2004-09-01
EP1247942B1 (de) 2006-06-28
DE60212751T2 (de) 2006-11-16
US6682300B2 (en) 2004-01-27
JP4191946B2 (ja) 2008-12-03
JP2003013705A (ja) 2003-01-15
ES2266330T3 (es) 2007-03-01
EP1247942A2 (de) 2002-10-09
CN1379166A (zh) 2002-11-13

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Legal Events

Date Code Title Description
AT Applications terminated before publication under section 16(1)